EP1693179A2 - Method of coupling a component to a fuel fill tube - Google Patents
Method of coupling a component to a fuel fill tube Download PDFInfo
- Publication number
- EP1693179A2 EP1693179A2 EP06250815A EP06250815A EP1693179A2 EP 1693179 A2 EP1693179 A2 EP 1693179A2 EP 06250815 A EP06250815 A EP 06250815A EP 06250815 A EP06250815 A EP 06250815A EP 1693179 A2 EP1693179 A2 EP 1693179A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- parison
- hot
- component
- mold
- filler neck
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 12
- 238000000034 method Methods 0.000 title claims description 29
- 230000008878 coupling Effects 0.000 title claims description 5
- 238000010168 coupling process Methods 0.000 title claims description 5
- 238000005859 coupling reaction Methods 0.000 title claims description 5
- 239000000945 filler Substances 0.000 claims description 67
- 239000000463 material Substances 0.000 claims description 46
- 230000013011 mating Effects 0.000 claims description 25
- 239000004698 Polyethylene Substances 0.000 claims description 6
- 238000000071 blow moulding Methods 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 6
- -1 polyethylene Polymers 0.000 claims description 6
- 229920000573 polyethylene Polymers 0.000 claims description 6
- 238000007664 blowing Methods 0.000 claims description 5
- 238000002844 melting Methods 0.000 claims description 4
- 230000008018 melting Effects 0.000 claims description 4
- DHKHKXVYLBGOIT-UHFFFAOYSA-N acetaldehyde Diethyl Acetal Natural products CCOC(C)OCC DHKHKXVYLBGOIT-UHFFFAOYSA-N 0.000 claims description 2
- 125000002777 acetyl group Chemical class [H]C([H])([H])C(*)=O 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims description 2
- 239000002828 fuel tank Substances 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/4242—Means for deforming the parison prior to the blowing operation
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/022—Particular heating or welding methods not otherwise provided for
- B29C65/028—Particular heating or welding methods not otherwise provided for making use of inherent heat, i.e. the heat for the joining comes from the moulding process of one of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1222—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a lapped joint-segment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/122—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section
- B29C66/1224—Joint cross-sections combining only two joint-segments, i.e. one of the parts to be joined comprising only two joint-segments in the joint cross-section comprising at least a butt joint-segment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/534—Joining single elements to open ends of tubular or hollow articles or to the ends of bars
- B29C66/5344—Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially annular, i.e. of finite length, e.g. joining flanges to tube ends
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/61—Joining from or joining on the inside
- B29C66/612—Making circumferential joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
- B29C66/7234—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a barrier layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/82—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps
- B29C66/826—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined
- B29C66/8266—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined
- B29C66/82661—Pressure application arrangements, e.g. transmission or actuating mechanisms for joining tools or clamps without using a separate pressure application tool, e.g. the own weight of the parts to be joined using fluid pressure directly acting on the parts to be joined by means of vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/832—Reciprocating joining or pressing tools
- B29C66/8322—Joining or pressing tools reciprocating along one axis
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K15/04—Tank inlets
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/10—Means for stopping flow from or in pipes or hoses
- F16L55/115—Caps
- F16L55/1157—Caps using hooks, pawls, or other movable or insertable locking members
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/001—Shaping in several steps
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/004—Shaping under special conditions
- B29C2791/006—Using vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/02—Combined blow-moulding and manufacture of the preform or the parison
- B29C49/04—Extrusion blow-moulding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/20—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor of articles having inserts or reinforcements ; Handling of inserts or reinforcements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/4242—Means for deforming the parison prior to the blowing operation
- B29C49/4244—Means for deforming the parison prior to the blowing operation during or after laying preform into the final mould
- B29C49/4245—Means for deforming the parison prior to the blowing operation during or after laying preform into the final mould aided by air floating
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/4273—Auxiliary operations after the blow-moulding operation not otherwise provided for
- B29C49/428—Joining
- B29C49/42806—Joining auxiliary parts to the article, e.g. handle
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7377—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
- B29C66/73773—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being semi-crystalline
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
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- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
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- B29K2023/00—Use of polyalkenes or derivatives thereof as moulding material
- B29K2023/04—Polymers of ethylene
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- B29K2059/00—Use of polyacetals, e.g. POM, i.e. polyoxymethylene or derivatives thereof, as moulding material
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/0079—Liquid crystals
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0065—Permeability to gases
- B29K2995/0067—Permeability to gases non-permeable
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- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0037—Other properties
- B29K2995/0068—Permeability to liquids; Adsorption
- B29K2995/0069—Permeability to liquids; Adsorption non-permeable
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- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
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- B29L2023/004—Bent tubes
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- B29L2031/00—Other particular articles
- B29L2031/712—Containers; Packaging elements or accessories, Packages
- B29L2031/7172—Fuel tanks, jerry cans
Definitions
- the present disclosure relates to blow-molding methods, and particularly to methods of coupling a component to an element formed in a blow mold. More particularly, the present disclosure relates to formation of a fuel tank filler neck using a blow-molding process.
- a component such as an inlet cup or inlet check valve is mated and bonded to a parison while the parison is located in a closed blow mold.
- the parison is formed in the blow mold to define a fuel tank filler neck in an illustrative embodiment.
- a vacuum is used to draw a hot parison into a mold cavity and inflation air is blown into a central passageway formed in the hot parison to inflate the parison in the mold cavity.
- a first filler neck component e.g., an inlet cup
- a first filler neck component is mated to a first end of the hot parison in the mold cavity to melt a portion of the first filler neck component and bond the first filler neck component to the first end of the hot parison.
- a second filler neck component (e.g., an inlet check valve) is mated to a second end of the hot parison in the mold cavity to melt a portion of the second filler neck component and bond the second filler neck component to the second end of the hot parison.
- Fig. 1 is a perspective view of a fuel tank coupled to a tank filler neck including an inlet cup and closure cap at an outer end of the filler neck and an inlet check valve at an inner end of the filler neck;
- Fig. 2 is a sectional view showing a "closed" blow mold in accordance with the present disclosure and showing an extruded uninflated parison located in a mold cavity formed between first and second mold dies and showing an inlet cup arranged to be mated with an upper end of the parison and an inlet check valve arranged to be mated with a lower end of the parison;
- Fig. 3 is a sectional view similar to Fig. 2 after "inflation air” has been blown into the closed blow mold to inflate the parison deployed in the mold cavity and showing the inlet cup after it has been mated with the upper end of the inflated parison and the inlet check valve after it has been mated with the lower end of the inflated parison;
- Fig. 4 is an enlarged sectional view showing a fixture moving toward the closed blow mold and carrying an inlet cup to be mated with an upper end of the inflated parison located in the closed blow mold;
- Fig. 5 is a view similar to Fig. 4 showing the inlet cup mated to the parison before withdrawal of the fixture from the inlet cup and from the closed blow mold;
- Fig. 6 is a view similar to Figs. 4 and 5 of another embodiment in accordance with the present disclosure wherein a vacuum is used to draw a parison to mate with an inlet cup positioned as an "insert" in a mold.
- a vehicle fuel system 10 comprises a fuel tank 12, a filler neck 14 having a lower end 16 coupled to fuel tank 12 and an upper end 18, and a removable closure cap 20 coupled to upper end 18 of filler neck 14 to close an open mouth 22 formed in the upper end of filler neck 14 as shown, for example, in Fig. 1.
- Vehicle fuel system 10 also comprises an inlet check valve 24 and an inlet cup 26 coupled to filler neck 14 as filler neck 14 is formed in a blow mold 28 using methods disclosed herein as suggested, for example, in Fig. 2 and 3.
- Inlet check valve 24 is configured to lie in a fuel-conducting passageway 15 formed in filler neck 14 and regulate flow of liquid fuel and fuel vapor therethrough.
- inlet check valve 24 includes a "one-way" valve member 30 that is slidable between a passageway-closing position shown in Fig. 1 and a passageway-opening position (not shown).
- a fuel-dispensing pump nozzle (not shown) contacts and moves valve member 30 inwardly against a yieldable biasing spring 32 to assume the opened position so that liquid fuel can flow past the one-way valve member 30 and into a fuel reservoir 34 provided in an interior region 36 of fuel tank 12.
- Inlet cup 26 includes a mount 38 and a nozzle restrictor 40 coupled to mount 38 and formed to include an aperture 42 as shown, for example, in Figs. 1 and 4.
- Mount 38 is coupled to outer end 18 of filler neck 14 by any suitable means and is sized to receive an inner portion of closure cap 20 therein.
- Aperture 42 is sized to receive a dispensing portion of a pump nozzle (not shown) therein during tank refueling.
- a hot extruded uninflated parison 44 is drawn using a vacuum 46 through an elongated mold cavity 48 defined by first and second mold dies 51, 52.
- These mold dies 51, 52 are included in blow mold 28 and are shown in a "closed” position in Figs. 2-5. It is within the scope of the present disclosure to apply vacuum 46 to elongated mold cavity 48 via either first opening 48' or second opening 48 ".
- inflation air 50 is blown into a central passageway 54 formed in hot extruded parison 44 to inflate parison 44 while parison 44 is deployed in the closed mold cavity 48.
- inflation air 50 expands the thin-walled hot-extruded parison 44 in radially outwardly extending directions to mate with half-round surfaces 151, 152 (or any other suitable surfaces) formed in first and second mold dies 51, 52.
- a component such as inlet check valve 24, inlet cup 26, or other suitable element is mated with parison 44 as suggested in Fig. 3 to cause a portion of the component contacting the hot parison 44 to "melt" so that a bond will develop between parison 44 and the mating component as the "hot” materials comprising parison 44 and the mating component solidify as they cool.
- Means is provided for moving a component to mate with a portion of a hot parison 44 to cause a bond to be established between parison 44 and that component.
- a fixture 60 is provided to carry inlet cup 26 into open mouth 62 of the inflated, hot, extruded parison 44 and hold inlet cup 26 in open mouth 62 until the plastics material comprising mount 38 of inlet cup 26 bonds to parison 44.
- fixture 60 is withdrawn, leaving inlet cup 26 mated with inflated parison 44 as shown, for example, in Fig. 3.
- parison 44 is made of polyarylamide (PAA). Parison 44 could also be made of liquid crystalline polyethylene (LCP). PAA is suitable for blow-molding. LCP is a low-permeation material suitable for blow-molding. Exterior portions of mount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to make parison 44.
- PAA polyarylamide
- LCP liquid crystalline polyethylene
- Exterior portions of mount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to make parison 44.
- mount 38 of inlet cup 26 is made of polyethylene or a combination of polyethylene and acetal. It is within the scope of this disclosure to position inlet cup 26 as an insert in a mold 70 and draw a vacuum 72 using vacuum supply 74 through inlet cup 26 via openings formed in nozzle restrictor 40 to move parison 44 in direction 76 to mate inlet cup 26 to a parison in the mold as suggested diagrammatically in Fig. 6.
- inlet cup 26 By mating and bonding a component such as inlet cup 26 to parison 44 while parison 44 is located in a closed mold 28, secondary processes are not needed to couple an inlet cup to a filler neck after the filler neck is removed from a mold.
- Inlet cup 26 is mated and bonded to parison 44 to yield a more robust joint or union between inlet cup 26 and parison 44.
- An o-ring seal between inlet cup 26 and filler neck 14 may or may not be needed.
- a method of coupling a component to a fuel fill tube in accordance with the present disclosure comprises the steps of providing an elongated mold cavity 48 between a first mold die 51 mated to a second mold die 52, and using a vacuum 46 to draw a hot extruded parison 44 into elongated mold cavity 48 as suggested in Fig. 2.
- Hot extruded parison 44 is formed to include opposite first and second ends 47, 49 and a central passageway 54 extending therethrough between first and second ends 47, 49.
- the present method further comprises the steps of blowing inflation air 50 through an opening 47' formed in first end 47 into central passageway 54 to inflate hot extruded parison 44 while hot extruded parison 44 is located in elongated mold cavity 48 and mating a first filler neck component 26 to first end 47 of hot extruded parison 44 after inflation of hot extruded parison 44. It is also within the scope of the present disclosure to blow inflation air 50 through an opening 49' formed in second end 49 to enlarge opening 47' in first end 47 to receive first filler neck component 26 therein.
- the mating step occurs while parison material comprising hot extruded parison 44 that has been heated to a hot temperature above a melting point of component material comprising first filler neck component 26 to (1) transfer heat associated with hot extruded parison 44 to first filler neck component 26 to melt some of the component material included in first filler neck component 26 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and first filler neck component 26 as hot extruded parison 44 and first filler neck component 26 cool to anchor first filler neck component 26 to the parison 44.
- the mating step further comprises the steps of mounting first filler neck component 26 on a fixture 60 and moving fixture 60 into central passageway 54 formed in hot extruded parison 44 through an opening 47' formed in first end 47 of hot extruded parison 44 to deposit a portion of the first filler neck component 26 in the central passage to facilitate transfer of heat from parison material in hot extruded parison 44 to component material of first filler neck component 26' located in central passageway 54 of hot extruded parison 44 as suggested in Figs. 4 and 5.
- the mating step further comprises the step of separating fixture 60 from first filler neck component 26 after parison 44 and component materials have cooled and bonded to anchor first filler neck component 26 to parison 44.
- the using step further comprises the steps of introducing a hot extruded parison 44 into elongated mold cavity 48 through a first cavity inlet 48' formed in one end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 and applying a vacuum 46 to hot extruded parison 44 through a second cavity inlet 48" formed in an opposite end of elongated mold cavity 48 while first mold die 51 is mated to second mold die 52 to move hot extruded parison through elongated mold cavity 48 in a direction 55 toward second cavity inlet 48 " as suggested in Fig. 2.
- the applying step ends before the blowing step begins in an illustrative embodiment. Inflation air 50 is blown through first cavity inlet 48' into central passageway 54 of hot extruded parison 44.
- a second filler neck component 24 is mated to second end 49 of hot extruded parison 44 after inflation of hot extruded parison 44 as suggested in Figs. 2 and 3.
- This mating step occurs while parison material comprising the hot extruded parison has been heated to a hot temperature above a melting point of component material comprising second filler neck component 24 to (1) transfer heat associated with hot extruded parison 44 to second filler neck component 24 to melt some of the component material included in second filler neck component 24 and (2) cause said some of the component material to mate with parison material in hot extruded parison 44 so that a bond develops between mating portions of hot extruded parison 44 and second filler neck component 24 as hot extruded parison 44 and second filler neck component 24 cool to anchor second filler neck component 24 to parison 44. It is within the scope of the present disclosure to blow inflation air 50 through opening 49' formed in second end 49 of parison 44 to enlarge opening 49' to
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Abstract
Description
- This application claims priority under 35 U.S.C. § 119(e) to U.S. Provisional Application Serial No. 60/653,833, filed February 17, 2005, which is expressly incorporated by reference herein.
- The present disclosure relates to blow-molding methods, and particularly to methods of coupling a component to an element formed in a blow mold. More particularly, the present disclosure relates to formation of a fuel tank filler neck using a blow-molding process.
- In accordance with the present disclosure, a component such as an inlet cup or inlet check valve is mated and bonded to a parison while the parison is located in a closed blow mold. The parison is formed in the blow mold to define a fuel tank filler neck in an illustrative embodiment.
- In accordance with one illustrative method, a vacuum is used to draw a hot parison into a mold cavity and inflation air is blown into a central passageway formed in the hot parison to inflate the parison in the mold cavity. A first filler neck component (e.g., an inlet cup) is mated to a first end of the hot parison in the mold cavity to melt a portion of the first filler neck component and bond the first filler neck component to the first end of the hot parison. A second filler neck component (e.g., an inlet check valve) is mated to a second end of the hot parison in the mold cavity to melt a portion of the second filler neck component and bond the second filler neck component to the second end of the hot parison.
- Features of the present disclosure will become apparent to those skilled in the art upon consideration of the following detailed description of illustrative embodiments exemplifying the best mode of carrying out the disclosure as presently perceived.
- The detailed description particularly refers to the accompanying figures in which:
- Fig. 1 is a perspective view of a fuel tank coupled to a tank filler neck including an inlet cup and closure cap at an outer end of the filler neck and an inlet check valve at an inner end of the filler neck;
- Fig. 2 is a sectional view showing a "closed" blow mold in accordance with the present disclosure and showing an extruded uninflated parison located in a mold cavity formed between first and second mold dies and showing an inlet cup arranged to be mated with an upper end of the parison and an inlet check valve arranged to be mated with a lower end of the parison;
- Fig. 3 is a sectional view similar to Fig. 2 after "inflation air" has been blown into the closed blow mold to inflate the parison deployed in the mold cavity and showing the inlet cup after it has been mated with the upper end of the inflated parison and the inlet check valve after it has been mated with the lower end of the inflated parison;
- Fig. 4 is an enlarged sectional view showing a fixture moving toward the closed blow mold and carrying an inlet cup to be mated with an upper end of the inflated parison located in the closed blow mold;
- Fig. 5 is a view similar to Fig. 4 showing the inlet cup mated to the parison before withdrawal of the fixture from the inlet cup and from the closed blow mold; and
- Fig. 6 is a view similar to Figs. 4 and 5 of another embodiment in accordance with the present disclosure wherein a vacuum is used to draw a parison to mate with an inlet cup positioned as an "insert" in a mold.
- A
vehicle fuel system 10 comprises afuel tank 12, afiller neck 14 having alower end 16 coupled tofuel tank 12 and anupper end 18, and a removable closure cap 20 coupled toupper end 18 offiller neck 14 to close an open mouth 22 formed in the upper end offiller neck 14 as shown, for example, in Fig. 1.Vehicle fuel system 10 also comprises aninlet check valve 24 and aninlet cup 26 coupled tofiller neck 14 asfiller neck 14 is formed in ablow mold 28 using methods disclosed herein as suggested, for example, in Fig. 2 and 3. -
Inlet check valve 24 is configured to lie in a fuel-conductingpassageway 15 formed infiller neck 14 and regulate flow of liquid fuel and fuel vapor therethrough. In the illustrated embodiment,inlet check valve 24 includes a "one-way"valve member 30 that is slidable between a passageway-closing position shown in Fig. 1 and a passageway-opening position (not shown). During refueling, liquid fuel discharged into an "open"filler neck 14 by a fuel-dispensing pump nozzle (not shown) contacts and movesvalve member 30 inwardly against ayieldable biasing spring 32 to assume the opened position so that liquid fuel can flow past the one-way valve member 30 and into afuel reservoir 34 provided in aninterior region 36 offuel tank 12. Reference is made to U.S. Patent No. 5,568,828 and Application No. 10/810,982, filed March 26, 2004, for disclosures relating to vehicle fuel systems and inlet check valves, which patent and application are hereby incorporated by reference herein. -
Inlet cup 26 includes amount 38 and anozzle restrictor 40 coupled tomount 38 and formed to include anaperture 42 as shown, for example, in Figs. 1 and 4. Mount 38 is coupled toouter end 18 offiller neck 14 by any suitable means and is sized to receive an inner portion of closure cap 20 therein.Aperture 42 is sized to receive a dispensing portion of a pump nozzle (not shown) therein during tank refueling. - As suggested, for example, in Fig. 2, a hot extruded
uninflated parison 44 is drawn using avacuum 46 through anelongated mold cavity 48 defined by first and second mold dies 51, 52. These mold dies 51, 52 are included inblow mold 28 and are shown in a "closed" position in Figs. 2-5. It is within the scope of the present disclosure to applyvacuum 46 toelongated mold cavity 48 via either first opening 48' orsecond opening 48 ". - As suggested in Figs. 2 and 3,
inflation air 50 is blown into acentral passageway 54 formed in hotextruded parison 44 to inflateparison 44 whileparison 44 is deployed in the closedmold cavity 48. As suggested, for example, in Fig. 3,inflation air 50 expands the thin-walled hot-extrudedparison 44 in radially outwardly extending directions to mate with half-round surfaces 151, 152 (or any other suitable surfaces) formed in first and second mold dies 51, 52. Whileparison 44 is hot, a component such asinlet check valve 24,inlet cup 26, or other suitable element is mated withparison 44 as suggested in Fig. 3 to cause a portion of the component contacting thehot parison 44 to "melt" so that a bond will develop betweenparison 44 and the mating component as the "hot"materials comprising parison 44 and the mating component solidify as they cool. - Means is provided for moving a component to mate with a portion of a
hot parison 44 to cause a bond to be established betweenparison 44 and that component. As suggested, for example, in Figs. 4 and 5, afixture 60 is provided to carryinlet cup 26 intoopen mouth 62 of the inflated, hot, extrudedparison 44 and holdinlet cup 26 inopen mouth 62 until the plasticsmaterial comprising mount 38 ofinlet cup 26 bonds toparison 44. After cooling has been completed,fixture 60 is withdrawn, leavinginlet cup 26 mated with inflatedparison 44 as shown, for example, in Fig. 3. - In an illustrative embodiment,
parison 44 is made of polyarylamide (PAA). Parison 44 could also be made of liquid crystalline polyethylene (LCP). PAA is suitable for blow-molding. LCP is a low-permeation material suitable for blow-molding. Exterior portions ofmount 38 can be made of PAA, LCP, or some suitable material that bonds to PAA, LCP, or the material used to makeparison 44. - In other embodiments,
mount 38 ofinlet cup 26 is made of polyethylene or a combination of polyethylene and acetal. It is within the scope of this disclosure to positioninlet cup 26 as an insert in amold 70 and draw avacuum 72 usingvacuum supply 74 throughinlet cup 26 via openings formed innozzle restrictor 40 to moveparison 44 indirection 76 to mateinlet cup 26 to a parison in the mold as suggested diagrammatically in Fig. 6. - By mating and bonding a component such as
inlet cup 26 toparison 44 whileparison 44 is located in a closedmold 28, secondary processes are not needed to couple an inlet cup to a filler neck after the filler neck is removed from a mold.Inlet cup 26 is mated and bonded toparison 44 to yield a more robust joint or union betweeninlet cup 26 andparison 44. An o-ring seal betweeninlet cup 26 andfiller neck 14 may or may not be needed.
A method of coupling a component to a fuel fill tube in accordance with the present disclosure comprises the steps of providing anelongated mold cavity 48 between a first mold die 51 mated to asecond mold die 52, and using avacuum 46 to draw a hot extrudedparison 44 intoelongated mold cavity 48 as suggested in Fig. 2. Hotextruded parison 44 is formed to include opposite first andsecond ends central passageway 54 extending therethrough between first andsecond ends
The present method further comprises the steps of blowinginflation air 50 through an opening 47' formed infirst end 47 intocentral passageway 54 to inflate hot extrudedparison 44 while hot extrudedparison 44 is located inelongated mold cavity 48 and mating a firstfiller neck component 26 tofirst end 47 of hot extrudedparison 44 after inflation of hot extrudedparison 44. It is also within the scope of the present disclosure to blowinflation air 50 through an opening 49' formed insecond end 49 to enlarge opening 47' infirst end 47 to receive firstfiller neck component 26 therein. The mating step occurs while parison material comprising hotextruded parison 44 that has been heated to a hot temperature above a melting point of component material comprising firstfiller neck component 26 to (1) transfer heat associated with hot extrudedparison 44 to firstfiller neck component 26 to melt some of the component material included in firstfiller neck component 26 and (2) cause said some of the component material to mate with parison material in hotextruded parison 44 so that a bond develops between mating portions of hot extrudedparison 44 and firstfiller neck component 26 as hot extrudedparison 44 and firstfiller neck component 26 cool to anchor firstfiller neck component 26 to theparison 44.
The mating step further comprises the steps of mounting firstfiller neck component 26 on afixture 60 and movingfixture 60 intocentral passageway 54 formed in hotextruded parison 44 through an opening 47' formed infirst end 47 of hotextruded parison 44 to deposit a portion of the firstfiller neck component 26 in the central passage to facilitate transfer of heat from parison material in hotextruded parison 44 to component material of first filler neck component 26' located incentral passageway 54 of hot extrudedparison 44 as suggested in Figs. 4 and 5. The mating step further comprises the step of separatingfixture 60 from firstfiller neck component 26 afterparison 44 and component materials have cooled and bonded to anchor firstfiller neck component 26 toparison 44. - The using step further comprises the steps of introducing a hot extruded
parison 44 intoelongated mold cavity 48 through a first cavity inlet 48' formed in one end ofelongated mold cavity 48 whilefirst mold die 51 is mated tosecond mold die 52 and applying avacuum 46 to hot extrudedparison 44 through asecond cavity inlet 48" formed in an opposite end ofelongated mold cavity 48 whilefirst mold die 51 is mated to second mold die 52 to move hot extruded parison throughelongated mold cavity 48 in adirection 55 towardsecond cavity inlet 48 " as suggested in Fig. 2. The applying step ends before the blowing step begins in an illustrative embodiment.Inflation air 50 is blown through first cavity inlet 48' intocentral passageway 54 of hot extrudedparison 44. - A second
filler neck component 24 is mated tosecond end 49 of hot extrudedparison 44 after inflation of hot extrudedparison 44 as suggested in Figs. 2 and 3. This mating step occurs while parison material comprising the hot extruded parison has been heated to a hot temperature above a melting point of component material comprising secondfiller neck component 24 to (1) transfer heat associated with hot extrudedparison 44 to secondfiller neck component 24 to melt some of the component material included in secondfiller neck component 24 and (2) cause said some of the component material to mate with parison material in hotextruded parison 44 so that a bond develops between mating portions of hot extrudedparison 44 and secondfiller neck component 24 as hotextruded parison 44 and secondfiller neck component 24 cool to anchor secondfiller neck component 24 to parison 44. It is within the scope of the present disclosure to blowinflation air 50 through opening 49' formed insecond end 49 ofparison 44 to enlarge opening 49' to receive secondfiller neck component 24 therein.
Claims (20)
- A method of coupling a component to a fuel fill tube, the method comprising the steps ofproviding an elongated mold cavity between a first mold die mated to a second mold die,using a vacuum to draw a hot extruded parison into the elongated mold cavity, the hot extruded parison being formed to include opposite first and second ends and a central passageway extending therethrough between the first and second ends,blowing inflation air into the central passageway to inflate the hot extruded parison while the hot extruded parison is located in the elongated mold cavity, andmating a first filler neck component to the first end of the hot extruded parison after inflation of the hot extruded parison, while parison material comprising the hot extruded parison that has been heated to a hot temperature above a melting point of component material comprising the first filler neck component, to transfer heat associated with the hot extruded parison to the first filler neck component to melt some of the component material included in the first filler neck component and cause said some of the component material to mate with parison material in the first end of the hot extruded parison so that a bond develops between mating portions of the hot extruded parison and the first filler neck component as the hot extruded parison and the first filler neck component cool to anchor the first filler neck component to the first end of the parison.
- The method of claim 1, further comprising the step of mating a second filler neck component to the second end of the hot extruded parison after inflation of the hot extruded parison, while parison material comprising the hot extruded parison that has been heated to a hot temperature above a melting point of component material comprising the second filler neck component, to transfer heat associated with the hot extruded parison to the second filler neck component to melt some of the component material included in the second filler neck component and cause said some of the component material to mate with parison material in the second end of the hot extruded parison so that a bond develops between mating portions of the hot extruded parison and the second filler neck component as the hot extruded parison and the second filler neck component cool to anchor the second filler neck component to the second end of the parison.
- The method of claim 1, wherein the mating step further comprises the steps of mounting the first filler neck component on a fixture and moving the fixture into the central passageway formed in the hot extruded parison through an opening formed in the first end of the hot extruded parison to deposit a portion of the first filler neck component in the central passage to facilitate transfer of heat from parison material in the hot extruded parison to component material of the first filler neck component located in the central passageway of the hot extruded parison.
- The method of claim 3, wherein the mating step further comprises the step of separating the fixture from the first filler neck component after the parison and component materials have cooled and bonded to anchor the first filler neck component to the parison.
- The method of claim 1, wherein the using step further comprises the steps of introducing a hot extruded parison into the elongated mold cavity through a first cavity inlet formed in one end of the elongated mold cavity while the first mold die is mated to the second mold die and applying a vacuum to the hot extruded parison through a second cavity inlet formed in an opposite end of the elongated mold cavity while the first mold die is mated to the second mold die to move the hot extruded parison through the elongated mold cavity in a direction toward the second cavity inlet.
- The method of claim 5, wherein the applying step ends before the blowing step begins and wherein inflation air is blown through the first cavity inlet into the central passageway of the hot extruded parison.
- The method of claim 1, wherein each of the first and second mold dies include a half-round surface forming a boundary portion of the elongated mold cavity and wherein the inflation air expands the hot extruded parison in radially outwardly extending directions to mate with the half-round surfaces of the first and second mold dies while the first mold die is mated with the second mold die.
- The method of claim 7, wherein the mating step further comprises the steps of mounting the first filler neck component on a fixture and moving the fixture into the central passageway formed in the hot extruded parison through an opening formed in the second end of the hot extruded parison to deposit a portion of the first filler neck in the central passage to facilitate transfer of heat from parison material in the hot extruded parison to component material of the first filler neck component located in the central passageway of the hot extruded parison.
- The method of claim 8, wherein the mating step further comprises the step of separating the fixture from the first filler neck component after the parison and component materials have cooled and bonded to anchor the filler neck component to the parison.
- A method of coupling a component to an element formed in a blow mold, the method comprising the steps ofproviding a first component andbonding the first component to a hot parison while the hot parison is located in a closed blow mold.
- The method of claim 10, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity between the mold dies, the first and second mold dies each including a surface facing toward the hot parison and the other mold die, and the bonding step further comprises the steps of inflating the hot parison in radially outwardly extending directions to mate with the surfaces formed in the first and second mold dies and, while the parison is still hot, mating the first component with the hot parison to cause a portion of the first component contacting the hot parison to melt so that a bond develops between the hot parison and the first component as hot materials comprising the parison and the first component solidify as they cool.
- The method of claim 11, wherein the bonding step further comprises providing means for moving the first component to mate with the hot parison to cause the bond to be established between the hot parison and the first component, the moving means carrying the first component into an open mouth of the inflated, hot parison and holding the first component in the open mouth until material comprising a mount of the first component bonds to the hot parison and, after a cooling has been completed, the moving means is withdrawn, leaving the first component mated to and bonded with the inflated parison.
- The method of claim 12, wherein the first component is an inlet cup including a mount and a nozzle restrictor coupled to the mount and formed to include an aperture, and exterior portions of the mount are made of a low-permeation material that bonds to a low-permeation material used to make the hot parison.
- The method of claim 13, wherein the low-permeation material of the exterior portions of the mount and the low-permeation material used to make the hot parison includes liquid crystalline polyethylene.
- The method of claim 10, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold, and the bonding step further comprises the steps of drawing the hot parison using a vacuum through an elongated mold cavity defined by the first and second mold dies, and the bonding step further comprises the step of blowing inflation air into a central passageway formed in the hot parison to inflate the hot parison while the hot parison is deployed in the mold cavity, the inflation air expanding the hot parison in radially outwardly extending directions to mate with half-round surfaces formed in the first and second mold dies, and while the parison is hot, the first component is mated with the hot parison to cause a portion of the first component contacting the hot parison to melt so that a bond will develop between the hot parison and the first component as materials comprising the hot parison and the first component solidify as they cool.
- The method of claim 15, wherein the materials comprising the hot parison and the first component include low-permeation materials suitable for blow-molding.
- The method of claim 1, further comprising the step of providing a second component and wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity therebetween, the first and second mold dies each including a surface facing toward the hot parison and the other mold die, and the bonding step further comprises the steps of inflating the hot parison in radially outwardly extending directions to mate with the surfaces formed in the first and second mold dies and, while the parison is hot, mating the first component with an upper end of the hot parison and mating the second component with a lower end of the hot parison to cause a portion of the first and second components contacting the hot parison to melt so that a bond develops between the hot parison and each of the first and second components as hot materials comprising the parison and the first and second components solidify as they cool.
- The method of claim 17, wherein the first component is an inlet cup, the second component is an inlet check valve, and the materials comprising the hot parison, the inlet cup, and the inlet check valve include low-permeation materials suitable for blow molding and suitable for bonding the inlet cup and the inlet check valve to the hot parison.
- The method of claim 18, wherein the inlet cup is made of one or more of polyethylene and acetal, and the hot parison is made of liquid crystalline polyethylene.
- The method of claim 1, wherein the bonding step comprises the step of providing first and second mold dies lying in mating relation to one another and cooperating to form a portion of the closed blow mold and a mold cavity between the mold dies, the first and second mold dies each including a surface facing toward the other mold die, and the bonding step further comprises the steps of positioning the first component as an insert in the closed blow mold and drawing a vacuum through the first component to mate the first component to the hot parison in the closed blow mold.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US65383305P | 2005-02-17 | 2005-02-17 |
Publications (3)
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EP1693179A2 true EP1693179A2 (en) | 2006-08-23 |
EP1693179A3 EP1693179A3 (en) | 2008-02-13 |
EP1693179B1 EP1693179B1 (en) | 2010-09-15 |
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Application Number | Title | Priority Date | Filing Date |
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EP06250815A Expired - Fee Related EP1693179B1 (en) | 2005-02-17 | 2006-02-16 | Method of coupling a component to a fuel fill tube |
Country Status (4)
Country | Link |
---|---|
US (2) | US7556067B2 (en) |
EP (1) | EP1693179B1 (en) |
CA (1) | CA2536862A1 (en) |
DE (1) | DE602006016881D1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2236267A1 (en) * | 2009-03-30 | 2010-10-06 | Geiger Automotive GmbH | Method and device for producing a plastic component and plastic component |
Families Citing this family (17)
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US20070261752A1 (en) * | 2006-04-13 | 2007-11-15 | Stant Manufacturing Inc. | Multiple-layer fluid fuel apparatus |
US8980161B2 (en) | 2007-03-06 | 2015-03-17 | Mercury Plastics, Inc. | Method for making a reservoir |
US8431067B2 (en) * | 2007-03-06 | 2013-04-30 | Mercury Plastics, Inc. | Method for making a reservoir |
DE202009001201U1 (en) * | 2009-01-31 | 2009-05-20 | Norma Germany Gmbh | Tankstutzen |
US8413431B2 (en) * | 2009-06-30 | 2013-04-09 | Eaton Corporation | Tank assembly |
GB2505053B (en) * | 2012-06-21 | 2018-09-05 | Mercury Plastics Inc | Method for making a reservoir |
DE102012022395A1 (en) * | 2012-11-16 | 2014-05-22 | Illinois Tool Works Inc. | Method for producing a fuel filling system for a motor vehicle and fuel filling system for a motor vehicle |
DE102013107978A1 (en) | 2013-07-25 | 2015-01-29 | Contitech Mgw Gmbh | Method for producing a media line with an end piece for receiving a component of a coupling |
JP6405508B2 (en) * | 2013-11-25 | 2018-10-17 | 三桜工業株式会社 | Fuel supply device and method of assembling the same |
US9873320B2 (en) | 2015-04-09 | 2018-01-23 | Stant Usa Corp. | Fuel tank pressure regulator |
US9902258B2 (en) | 2015-04-27 | 2018-02-27 | Stant Usa Corp. | Fuel tank pressure regulator |
US10458366B2 (en) | 2016-10-31 | 2019-10-29 | Stant Usa Corp. | Fuel tank pressure regulator |
DE212018000084U1 (en) | 2017-03-01 | 2019-05-09 | Stant Usa Corp. | Kraftstofftankeinfüllrohranordnung |
EP3385105B1 (en) * | 2017-04-06 | 2019-04-03 | Magna Steyr Fuel Systems GesmbH | Refuelling device |
US10794335B2 (en) | 2018-06-01 | 2020-10-06 | Stant Usa Corp. | Fuel tank pressure regulator |
CN111059366A (en) * | 2018-10-16 | 2020-04-24 | 湖南易净环保科技有限公司 | Continuous fiber reinforced thermoplastic pipeline and production method thereof |
US11215147B2 (en) | 2020-02-14 | 2022-01-04 | Stant Usa Corp. | Fuel tank pressure regulator |
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2006
- 2006-02-15 US US11/276,146 patent/US7556067B2/en active Active
- 2006-02-15 US US11/276,148 patent/US20060180959A1/en not_active Abandoned
- 2006-02-16 EP EP06250815A patent/EP1693179B1/en not_active Expired - Fee Related
- 2006-02-16 DE DE602006016881T patent/DE602006016881D1/en active Active
- 2006-02-16 CA CA002536862A patent/CA2536862A1/en not_active Abandoned
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US5308427A (en) | 1992-09-28 | 1994-05-03 | Ford Motor Company | Method for fastening plastic articles |
US5568828A (en) | 1994-11-30 | 1996-10-29 | Stant Manufacturing Inc. | Fuel-delivery control system |
JP4179528B2 (en) | 2001-05-23 | 2008-11-12 | 株式会社デンソー | Secondary battery inspection method |
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EP2236267A1 (en) * | 2009-03-30 | 2010-10-06 | Geiger Automotive GmbH | Method and device for producing a plastic component and plastic component |
Also Published As
Publication number | Publication date |
---|---|
US20060180241A1 (en) | 2006-08-17 |
EP1693179B1 (en) | 2010-09-15 |
US20060180959A1 (en) | 2006-08-17 |
DE602006016881D1 (en) | 2010-10-28 |
US7556067B2 (en) | 2009-07-07 |
CA2536862A1 (en) | 2006-08-17 |
EP1693179A3 (en) | 2008-02-13 |
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